Master advanced CAD design through Python scripting, create mathematically-perfect gears, generate lattice structures, optimize designs iteratively, and automate workflows that would take hours manually. Unlock FreeCAD’s true computational power. #PythonCAD #GenerativeDesign #ParametricOptimization
🎯 Learning Objectives
By the end of this lesson, you will be able to:
Understand when Python scripting is superior to GUI-based CAD modeling
Write Python scripts to generate complex parametric geometry algorithmically
Create lattice structures and generative designs impossible to model manually
Implement design optimization loops that explore parameter spaces automatically
Automate batch operations and data-driven design workflows
Apply Python CAD to real research and engineering problems
🔧 Why Python Scripting in CAD?
Whi le GU I-bas ed CA D is perf ect for manu ally desig ning indiv idual par ts, Pyt hon scrip ting unlo cks an enti rely diffe rent capab ility: algori thmic des ign. Inst ead of draw ing geom etry, yo u def ine mathem atical rul es th at gene rate geom etry. Th is enab les des ign explor ation, optimi zation, and compl exity th at would be imprac tical or impos sible with mou se and keyb oard alo ne.
When Python Beats GUI
Problem: Design a mathematically-perfect involute gear
GUI Approach:
Manually calculate dozens of tooth profile points
Sketch each curve segment individually
Repeat for every tooth
Any parameter change = start over
Time: Hours, error-prone
Python Approach:
Define involute equation
Loop to generate all teeth
Parameters control everything
Regenerate in seconds
Time: Minutes, mathematically exact
Real Applications
Involute gears, cycloidal gears, bevel gears
NACA airfoils (precise aerodynamic profiles)
Spiral springs, compression springs with variable pitch
Bezier and B-spline surfaces from equations
Problem: Create a lattice structure for lightweight 3D-printed part
GUI Approach:
Model one lattice cell
Copy and pattern… but how many cells?
Modify for variable density?
Nearly impossible
Time: Impractical
Python Approach:
Define lattice mathematics (cubic, gyroid, Voronoi)
Loop through 3D space creating cells
Variable density = change loop conditions
Generate complex infill patterns
Time: Minutes
Real Applications
Aerospace: Lightweight structural components
Biomedical: Bone implants with controlled porosity
3D Printing: Custom infill for strength/weight optimization
Architecture: Complex facade patterns
Problem: Find optimal beam dimensions for minimum weight at target strength
GUI Approach:
Manually model variant 1
Test strength (FEA)
Manually adjust dimensions
Model variant 2, test…
Repeat 50 times?
Time: Days
Python Approach:
Loop: for width in range(10, 50, 2)
Generate geometry automatically
Run FEA in loop
Record results, find optimum
Test 100 variants in minutes
Time: Automated overnight
Real Applications
Structural optimization (topology, size, shape)
Heat sink fin spacing optimization
Airfoil shape optimization for drag
Mechanism kinematics optimization
Problem: Create housing for electronics from 3D scanned point cloud
GUI Approach:
Import 1000+ points
Manually sketch around them?
Impossible to maintain precision
Time: Impractical
Python Approach:
Import CSV/point cloud
Algorithmically fit surfaces
Generate geometry from measurements
Update when data changes
Time: Automated
Real Applications
Reverse engineering: Creating CAD from scans
Custom fit: Medical devices, prosthetics, orthotics
Sensor integration: Designing around real measurements
Research: Geometry from experimental data
Problem: Export technical drawings for 200-part assembly
GUI Approach:
Open each part
Create TechDraw page
Add views, dimensions
Export PDF
Repeat 200 times
Time: Days
Python Approach:
Loop through parts list
Auto-create drawings
Apply standard template
Export all
Time: Minutes (unattended)
Real Applications
Drawing automation for assemblies
Mass export (STL for 3D printing entire library)
BOM generation from assemblies
Quality control: Batch dimension checks
The Power Shift
💡 Paradigm Change
GUI CAD: You are the designer, you create every feature manually
Python CAD: You are the programmer, you teach the computer how to design
Result: The computer can now explore thousands of design variants, handle mathematical complexity you couldn’t calculate by hand, and automate workflows that would take weeks manually.
🐍 Part 1: FreeCAD Python Basics
Accessing Python in FreeCAD
Open FreeCAD Python Console
View → Panels → Python console
Bottom panel appears with >>> prompt
Try a simple command:
>>> print ( " Hello from FreeCAD Python! " )
Create a box:
>>> box = Part. makeBox ( 10 , 20 , 30 )
A 10×20×30mm box appears in 3D view!
Python Console vs. Macro Files
Use for:
Quick experiments
Testing commands
One-off operations
Learning the API
Limitations:
Commands lost when FreeCAD closes
Can’t easily rerun complex sequences
No loops/functions for complex logic
Use for:
Reusable scripts
Complex algorithms
Batch operations
Production workflows
Creating macros:
Macro → Macros… → Create
Enter name: MyScript.FCMacro
Click Edit (opens text editor)
Write Python code
Save
Execute to run
Macros are saved permanently and can be run anytime!
Use for:
Complex projects
Integration with other tools
Version control (Git)
Collaborative development
Running external scripts:
>>> exec ( open ( ' /path/to/script.py ' ) . read ())
Or use FreeCAD as a Python module in external scripts.
Essential FreeCAD Python Modules
📦 Core Modules You'll Use
Part - Basic solid geometry (boxes, cylinders, spheres, boolean operations)
FreeCAD - Document management, objects, parameters
Sketcher - Programmatic sketching (advanced)
Draft - 2D/3D drafting operations
Mesh - Mesh generation, STL operations
numpy - Numerical arrays, mathematics (if installed)
⚙️ Part 2: Algorithmic Design - Involute Gear Generator
Invo lute gea rs are the indu stry stan dard for pow er transm ission, us ed in autom otive transm issions, indus trial gearb oxes, and preci sion machi nery. Crea ting mathem atically-perf ect invo lute prof iles manu ally is tedi ous and err or-pro ne. Pyt hon gener ates th em flawl essly fr om equat ions.
Why Involute Gears?
Engineering advantages:
Constant velocity ratio (smooth power transmission)
Insensitive to center distance variations
Easy to manufacture
Standard tooth profiles (interchangeability)
Manual modeling challenges:
Involute curve is defined by integral equation
Each tooth requires dozens of precisely calculated points
Changing module or tooth count = complete redesign
Python solution: Define mathematics once, generate any gear instantly.
The Involute Equation
The involute of a circle is the curve traced by a point on a taut string unwinding from that circle.
Parametric equations:
Where:
is the base circle radius
is the unwinding angle parameter
Python Gear Generator
def create_involute_gear ( module , num_teeth , pressure_angle= 20 , thickness= 10 ) :
Generate a parametric involute spur gear.
- module: Gear module (pitch diameter / number of teeth) in mm
- num_teeth: Number of teeth
- pressure_angle: Pressure angle in degrees (typically 20°)
- thickness: Gear thickness in mm
Returns: FreeCAD Part object
# Calculate gear geometry
pitch_diameter = module * num_teeth
pitch_radius = pitch_diameter / 2.0
pressure_angle_rad = math. radians ( pressure_angle )
base_radius = pitch_radius * math. cos ( pressure_angle_rad )
addendum = module # Height above pitch circle
dedendum = 1.25 * module # Depth below pitch circle
outer_radius = pitch_radius + addendum
root_radius = pitch_radius - dedendum
tooth_angle = 2 * math.pi / num_teeth
# Generate one tooth profile
def involute_point ( theta ) :
""" Generate point on involute curve """
x = base_radius * (math. cos ( theta ) + theta * math. sin ( theta ))
y = base_radius * (math. sin ( theta ) - theta * math. cos ( theta ))
for tooth_num in range ( num_teeth ):
angle_offset = tooth_num * tooth_angle
# Generate involute curve points (from base circle to outer)
theta_end = math. sqrt ( (outer_radius / base_radius) ** 2 - 1 )
for i in range ( 20 ): # 20 points per involute curve
theta = theta_start + (theta_end - theta_start) * i / 19.0
x, y = involute_point ( theta )
# Rotate to tooth position
x_rot = x * math. cos ( angle_offset ) - y * math. sin ( angle_offset )
y_rot = x * math. sin ( angle_offset ) + y * math. cos ( angle_offset )
involute_points. append ( App. Vector ( x_rot , y_rot , 0 ))
# Create tooth profile wire
# (Simplified - real implementation would include root fillet, mirror, etc.)
tooth_curve = Part. BSplineCurve ()
tooth_curve. interpolate ( involute_points )
teeth_wires. append ( tooth_curve. toShape ())
# Create gear body (simplified - circular approximation)
# In production code, would build precise tooth profiles
gear_circle = Part. makeCircle ( pitch_radius )
gear_face = Part. Face ( Part. Wire ( gear_circle ))
gear_solid = gear_face. extrude ( App. Vector ( 0 , 0 , thickness ))
gear = create_involute_gear ( module = 2.5 , num_teeth = 24 , thickness = 10 )
Part. show ( gear , " InvoluteGear " )
print ( " ✓ Involute gear generated! " )
print ( f " Pitch diameter: { 2.5 * 24 } mm" )
print ( f " Number of teeth: 24" )
Key programming concepts:
Functions with parameters
def create_involute_gear ( module , num_teeth , ... ) :
Makes the code reusable—change parameters, get new gear!
Mathematical calculations
base_radius = pitch_radius * math. cos ( pressure_angle_rad )
Python handles complex gear mathematics automatically
Loops for generation
for tooth_num in range ( num_teeth ):
Generates all teeth—whether 10 or 100 teeth, same code!
Point-by-point curve building
involute_points. append ( App. Vector ( x_rot , y_rot , 0 ))
Builds curves from mathematical equations
Return FreeCAD object
Result is a normal FreeCAD Part—can use in assemblies!
Generate different gears:
# Small gear - Module 2, 18 teeth
gear_small = create_involute_gear ( module = 2.0 , num_teeth = 18 , thickness = 8 )
Part. show ( gear_small , " SmallGear " )
# Large gear - Module 3, 48 teeth
gear_large = create_involute_gear ( module = 3.0 , num_teeth = 48 , thickness = 12 )
Part. show ( gear_large , " LargeGear " )
# Fine pitch gear - Module 1.5, 30 teeth
gear_fine = create_involute_gear ( module = 1.5 , num_teeth = 30 , thickness = 6 )
Part. show ( gear_fine , " FinePitchGear " )
Design exploration - batch generate:
# Generate family of gears for testing
for teeth in [ 12 , 18 , 24 , 30 , 36 ] :
gear = create_involute_gear ( module = 2.5 , num_teeth = teeth , thickness = 10 )
Part. show ( gear , f "Gear_ {teeth} T" )
print ( f "Created gear with {teeth} teeth" )
Generates 5 different gears in seconds!
Manufacturing:
Generate entire gearbox worth of gears
Export to CNC for cutting
Precise profiles guarantee mesh quality
Research:
Study effect of pressure angle on contact stress
Generate test gears with deliberate profile modifications
Optimize tooth count for specific applications
Rapid prototyping:
3D print custom gears for robots, mechanisms
Iterate designs quickly
Test different ratios
Custom machinery:
Non-standard modules for special applications
Variable tooth spacing (non-uniform)
Integrated mounting features
🏗️ Part 3: Lattice Structure Generation
Latt ice struc tures are revolu tionizing lightw eight des ign in aeros pace, biome dical impl ants, and 3D prin ting. The se peri odic cell ular struc tures prov ide hi gh stre ngth-to-wei ght rat ios and contr olled poro sity—but crea ting th em manu ally in CA D is nea rly impos sible. Pyt hon mak es th em triv ial.
Why Lattice Structures?
Engineering benefits:
Aerospace Applications
Weight reduction: 50-70% lighter than solid parts at equivalent strength
Fuel efficiency: Every gram saved matters in aircraft/spacecraft
Vibration damping: Cellular structure absorbs vibrations
Heat dissipation: Increased surface area for cooling
Biomedical Applications
Bone ingrowth: Porosity allows bone cells to grow into implants
Modulus matching: Can tune stiffness to match natural bone
Reduced stress shielding: Prevents bone degradation around implants
Custom patient-fit: Generate structures matching CT scan data
3D Printing Applications
Material savings: Reduce print time and filament cost
Support structures: Easily removable, controlled density
Functional infill: Optimize strength/weight for specific loads
Thermal management: Heat sinks with optimized flow
Types of Lattice Structures
Simple orthogonal beams
Advantages:
Easy to analyze structurally
Predictable properties
Simple to generate
Disadvantages:
Stress concentrations at joints
Anisotropic (different strength in different directions)
Applications:
General lightweight structures
Architectural models
Educational demonstrations
Face-centered cubic with internal struts
Advantages:
Isotropic (uniform strength all directions)
Excellent strength-to-weight
Well-studied properties
Disadvantages:
More complex joints
Harder to manufacture
Applications:
Aerospace structural components
High-performance 3D printing
Sandwich panel cores
Smooth triply-periodic minimal surface
Advantages:
No stress concentrations (smooth surfaces)
Isotropic properties
High surface area
Beautiful aesthetics
Disadvantages:
Complex mathematics
Requires implicit surface meshing
Applications:
Bone implants (smooth promotes growth)
Heat exchangers (high surface area)
Filters and separators
Artistic/architectural elements
Python Cubic Lattice Generator
def create_cubic_lattice ( x_size , y_size , z_size , cell_size , strut_diameter ) :
Generate a cubic lattice structure.
- x_size, y_size, z_size: Overall dimensions in mm
- cell_size: Size of one cubic cell in mm
- strut_diameter: Diameter of lattice struts in mm
Returns: FreeCAD Part object
radius = strut_diameter / 2.0
# Calculate number of cells in each direction
nx = int ( x_size / cell_size ) + 1
ny = int ( y_size / cell_size ) + 1
nz = int ( z_size / cell_size ) + 1
# Generate X-direction struts
# Create cylinder along X-axis
start = App. Vector ( 0 , y_pos , z_pos )
end = App. Vector ( x_size , y_pos , z_pos )
strut = Part. makeCylinder ( radius , x_size , start , end - start )
# Generate Y-direction struts
start = App. Vector ( x_pos , 0 , z_pos )
end = App. Vector ( x_pos , y_size , z_pos )
strut = Part. makeCylinder ( radius , y_size , start , end - start )
# Generate Z-direction struts
start = App. Vector ( x_pos , y_pos , 0 )
end = App. Vector ( x_pos , y_pos , z_size )
strut = Part. makeCylinder ( radius , z_size , start , end - start )
# Fuse all struts into one solid
print ( f "Fusing { len ( struts ) } struts..." )
lattice = lattice. fuse ( strut )
print ( f "✓ Cubic lattice generated: {nx} × {ny} × {nz} cells" )
# Generate 50×50×50mm lattice with 5mm cells
lattice = create_cubic_lattice (
Part. show ( lattice , " CubicLattice " )
Variable Density Lattice
Real-world need: Bone implants need higher density at load-bearing surfaces, lower density in core.
def create_variable_density_lattice ( x_size , y_size , z_size , cell_size_func ) :
Generate lattice with variable cell size (density).
cell_size_func: Function that returns cell size given (x, y, z) position
# Adaptive cell generation
# Get local cell size based on position
local_cell_size = cell_size_func ( x , y , z )
# Generate strut at this location
# ... (strut generation code)
# Example: Denser at edges, sparser in center
def density_function ( x , y , z ) :
center_x, center_y, center_z = 25 , 25 , 25
distance_from_center = ((x - center_x) ** 2 + (y - center_y) ** 2 + (z - center_z) ** 2 ) ** 0.5
# Cell size increases toward center (lower density)
return 3 + distance_from_center / 10.0
lattice_var = create_variable_density_lattice ( 50 , 50 , 50 , density_function )
🔬 Part 4: Design Optimization Loop
Des ign optimi zation is the ho ly gra il of engine ering: automa tically find ing the be st des ign fr om thous ands of possib ilities. Pyt hon enab les itera tive explor ation of des ign spa ces—test ing vari ants, measu ring perfor mance, and conve rging on opti mal solut ions. Th is is adva nced CA D us ed in aeros pace, autom otive, and cutt ing-ed ge rese arch.
Optimization Problem Example
Engineering challenge: Design a lightweight bracket that can support 500N load with minimum weight.
Design variables:
Wall thickness (1-5mm)
Rib spacing (10-30mm)
Fillet radius (2-6mm)
Objective: Minimize mass
Constraints: Max stress < 150 MPa (material yield strength)
Python Optimization Framework
def create_bracket ( wall_thickness , rib_spacing , fillet_radius ) :
Generate parametric bracket geometry.
Returns: FreeCAD Part object and calculated mass
base = Part. makeBox ( 100 , 80 , wall_thickness )
wall = Part. makeBox ( wall_thickness , 80 , 50 )
wall. translate ( App. Vector ( 0 , 0 , wall_thickness ))
num_ribs = int ( 80 / rib_spacing )
for i in range ( 1 , num_ribs ):
App. Vector ( 0 , y_pos , wall_thickness ),
App. Vector ( 50 , y_pos , wall_thickness ),
# Create rib profile and extrude
rib_wire = Part. makePolygon ( rib_points + [ rib_points [ 0 ] ] )
rib_face = Part. Face ( rib_wire )
rib = rib_face. extrude ( App. Vector ( 0 , wall_thickness , 0 ))
bracket = base. fuse ( wall )
bracket = bracket. fuse ( rib )
# Apply fillets (if radius > 0)
# ... (identify edges to fillet)
# bracket = bracket.makeFillet(fillet_radius, edges_to_fillet)
# Calculate mass (assuming aluminum: 2700 kg/m³ = 2.7e-6 kg/mm³)
volume = bracket.Volume # mm³
density = 2.7e-6 # kg/mm³
mass = volume * density # kg
def run_fea_analysis ( bracket_part , load_force= 500 ) :
Run FEA simulation on bracket (simplified).
In real implementation, would use FreeCAD FEM workbench or external solver.
Returns: max_stress (MPa), max_deflection (mm)
# This is a simplified placeholder
# Real FEA would use FreeCAD's FEM workbench:
# analysis = ObjectsFem.makeAnalysis(App.ActiveDocument, "Analysis")
# mesh = ObjectsFem.makeMeshGmsh(App.ActiveDocument, "Mesh")
# mesh.Part = bracket_part
# mesh.CharacteristicLengthMax = 5.0
# # Apply constraints and loads
# # ... (fixed constraint, force)
# Simplified estimation for demonstration
# (Real code would integrate actual FEA)
max_stress = 100 + random. random () * 50 # Placeholder
max_deflection = 0.1 + random. random () * 0.5
return max_stress, max_deflection
def optimize_bracket_design () :
Explore design space and find optimal bracket.
wall_thicknesses = [ 1.0 , 1.5 , 2.0 , 2.5 , 3.0 ]
rib_spacings = [ 10 , 15 , 20 , 25 , 30 ]
fillet_radii = [ 0 , 2 , 4 , 6 ]
print ( " Starting optimization... " )
print ( f "Testing { len ( wall_thicknesses ) * len ( rib_spacings ) * len ( fillet_radii ) } variants" )
# Exhaustive search (for small design space)
# For large spaces, use genetic algorithms or gradient descent
for wall_t in wall_thicknesses:
for rib_s in rib_spacings:
for fillet_r in fillet_radii:
bracket, mass = create_bracket ( wall_t , rib_s , fillet_r )
max_stress, deflection = run_fea_analysis ( bracket )
stress_ok = max_stress < 150 # MPa limit
' wall_thickness ' : wall_t,
' fillet_radius ' : fillet_r,
' max_stress_MPa ' : max_stress,
' deflection_mm ' : deflection,
# Update best if feasible and lighter
if stress_ok and mass < best_mass:
print ( f "✓ New best: variant {variant_num} , mass= {mass :.3f } kg, stress= {max_stress :.1f } MPa" )
# Save results to CSV for analysis
with open ( ' optimization_results.csv ' , ' w ' , newline = '' ) as csvfile:
fieldnames = [ ' variant ' , ' wall_thickness ' , ' rib_spacing ' , ' fillet_radius ' ,
' mass_kg ' , ' max_stress_MPa ' , ' deflection_mm ' , ' feasible ' ]
writer = csv. DictWriter ( csvfile , fieldnames = fieldnames )
writer. writerows ( results )
print ( " OPTIMIZATION COMPLETE " )
print ( f " Wall thickness: {best_design [ ' wall_thickness ' ] } mm" )
print ( f " Rib spacing: {best_design [ ' rib_spacing ' ] } mm" )
print ( f " Fillet radius: {best_design [ ' fillet_radius ' ] } mm" )
print ( f " Mass: {best_design [ ' mass_kg ' ] :.3f } kg" )
print ( f " Max stress: {best_design [ ' max_stress_MPa ' ] :.1f } MPa" )
print ( f "Results saved to optimization_results.csv" )
return best_design, results
best_bracket, all_results = optimize_bracket_design ()
import matplotlib.pyplot as plt
def visualize_optimization_results ( results ) :
Create plots showing design space exploration.
df = pd. DataFrame ( results )
# Separate feasible and infeasible designs
feasible = df[df[ ' feasible ' ] == True ]
infeasible = df[df[ ' feasible ' ] == False ]
# Create figure with subplots
fig, axes = plt. subplots ( 2 , 2 , figsize = ( 12 , 10 ) )
# Plot 1: Mass vs. Wall Thickness
ax. scatter ( feasible [ ' wall_thickness ' ] , feasible [ ' mass_kg ' ] ,
c = ' green ' , label = ' Feasible ' , alpha = 0.6 )
ax. scatter ( infeasible [ ' wall_thickness ' ] , infeasible [ ' mass_kg ' ] ,
c = ' red ' , label = ' Overstressed ' , alpha = 0.3 )
ax. set_xlabel ( ' Wall Thickness (mm) ' )
ax. set_ylabel ( ' Mass (kg) ' )
# Plot 2: Stress vs. Mass (Pareto front)
ax. scatter ( feasible [ ' mass_kg ' ] , feasible [ ' max_stress_MPa ' ] ,
ax. axhline ( y = 150 , color = ' r ' , linestyle = ' -- ' , label = ' Stress limit ' )
ax. set_xlabel ( ' Mass (kg) ' )
ax. set_ylabel ( ' Max Stress (MPa) ' )
# Plot 3: Rib Spacing Effect
for rib_s in feasible[ ' rib_spacing ' ]. unique ():
subset = feasible[feasible[ ' rib_spacing ' ] == rib_s]
ax. plot ( subset [ ' wall_thickness ' ] , subset [ ' mass_kg ' ] ,
marker = ' o ' , label = f 'Rib spacing {rib_s} mm' )
ax. set_xlabel ( ' Wall Thickness (mm) ' )
ax. set_ylabel ( ' Mass (kg) ' )
# Plot 4: Design space heatmap
pivot = feasible. pivot_table ( values = ' mass_kg ' ,
columns = ' wall_thickness ' ,
im = ax. imshow ( pivot , cmap = ' RdYlGn_r ' , aspect = ' auto ' )
ax. set_xticks ( range ( len ( pivot.columns )))
ax. set_xticklabels ( pivot.columns )
ax. set_yticks ( range ( len ( pivot.index )))
ax. set_yticklabels ( pivot.index )
ax. set_xlabel ( ' Wall Thickness (mm) ' )
ax. set_ylabel ( ' Rib Spacing (mm) ' )
plt. colorbar ( im , ax = ax , label = ' Mass (kg) ' )
plt. savefig ( ' optimization_plots.png ' , dpi = 300 )
print ( " ✓ Plots saved to optimization_plots.png " )
# Generate visualizations
visualize_optimization_results ( all_results )
Real Research Applications
🔬 Research Case Studies
1. Topology Optimization for Aerospace Bracket
Challenge: Design lightest bracket for satellite structure
Method: Python + FEA in loop, remove material iteratively where stress is low
Result: 40% weight reduction while maintaining strength
Publication: Multiple papers in Journal of Mechanical Design
2. Bone Implant Porosity Optimization
Challenge: Match implant stiffness to natural bone to prevent stress shielding
Method: Python-generated lattice with variable density, FEA validation
Result: Custom implants with patient-specific porosity gradients
Impact: Clinical trials showing improved bone ingrowth
3. Heat Sink Fin Optimization
Challenge: Maximize heat dissipation with constrained airflow and size
Method: Python + CFD simulation loop, varying fin spacing/height
Result: 25% better cooling performance
Application: High-power LED thermal management
📊 Part 5: Data-Driven Design
Importing Measurement Data
Re al-wor ld engine ering oft en sta rts with measur ements—3D sca ns of par ts, sen sor da ta, experi mental resu lts, or pati ent-spec ific anat omy. Pyt hon brid ges the ga p betw een ra w da ta and param etric CA D mod els, enab ling reve rse engine ering, cus tom fitt ing, and da ta-info rmed des ign.
Use Case: Custom Enclosure from 3D Scan
Scenario: Design protective housing for electronics assembly measured via 3D scanning
def import_point_cloud ( csv_file ) :
Import point cloud from CSV file.
CSV format: x, y, z (coordinates in mm)
data = np. loadtxt ( csv_file , delimiter = ' , ' , skiprows = 1 )
# Create FreeCAD Points object
for i in range ( len ( x_coords )):
points. append ( App. Vector ( x_coords [ i ] , y_coords [ i ] , z_coords [ i ]))
# Create Points object in FreeCAD
point_cloud = App.ActiveDocument. addObject ( " Points::Feature " , " PointCloud " )
point_cloud.Points = points
print ( f "✓ Imported { len ( points ) } points from {csv_file} " )
# Import scanned electronics assembly
scanned_points = import_point_cloud ( ' electronics_scan.csv ' )
def create_bounding_enclosure ( points , clearance= 5.0 ) :
Create enclosure with specified clearance around point cloud.
- points: List of FreeCAD Vectors
- clearance: Minimum distance from points to enclosure walls (mm)
Returns: Enclosure Part object
x_coords = [ p.x for p in points ]
y_coords = [ p.y for p in points ]
z_coords = [ p.z for p in points ]
x_min, x_max = min ( x_coords ), max ( x_coords )
y_min, y_max = min ( y_coords ), max ( y_coords )
z_min, z_max = min ( z_coords ), max ( z_coords )
enclosure = Part. makeBox ( width , length , height ,
App. Vector ( x_min , y_min , z_min ))
print ( f "✓ Enclosure created: {width :.1f } × {length :.1f } × {height :.1f } mm" )
# Generate enclosure with 5mm clearance
enclosure = create_bounding_enclosure ( scanned_points , clearance = 5.0 )
Part. show ( enclosure , " Enclosure " )
from scipy.interpolate import griddata
def create_surface_from_points ( points , grid_resolution= 50 ) :
Fit smooth surface to point cloud using interpolation.
Useful for organic shapes, terrain, medical anatomy.
x = np. array ( [ p.x for p in points ] )
y = np. array ( [ p.y for p in points ] )
z = np. array ( [ p.z for p in points ] )
x_min, x_max = x. min (), x. max ()
y_min, y_max = y. min (), y. max ()
xi = np. linspace ( x_min , x_max , grid_resolution )
yi = np. linspace ( y_min , y_max , grid_resolution )
xi, yi = np. meshgrid ( xi , yi )
# Interpolate Z values on grid
zi = griddata ( (x, y) , z , (xi, yi) , method = ' cubic ' )
# Convert grid to FreeCAD BSpline surface
# ... (advanced - requires FreeCAD Part.BSplineSurface)
print ( " ✓ Surface fitted to point cloud " )
return None # Would return FreeCAD surface object
# Fit surface to scanned data
surface = create_surface_from_points ( scanned_points )
def add_mounting_holes ( enclosure , hole_positions ) :
Add mounting holes at specified locations.
hole_positions: List of (x, y) tuples
hole_diameter = 3.5 # M3 clearance
for x, y in hole_positions:
# Create hole through enclosure thickness
hole_pos = App. Vector ( x , y , - 10 ) # Below bottom
hole_dir = App. Vector ( 0 , 0 , 1 ) # Vertical
hole = Part. makeCylinder ( hole_diameter / 2 , 100 , hole_pos , hole_dir )
enclosure = enclosure. cut ( hole )
# Add mounting holes at corners
hole_positions = [ ( 10 , 10 ), ( 10 , 90 ), ( 90 , 10 ), ( 90 , 90 ) ]
enclosure_with_holes = add_mounting_holes ( enclosure , hole_positions )
Part. show ( enclosure_with_holes , " FinalEnclosure " )
Research Application: Patient-Specific Medical Devices
Workflow:
Acquire CT/MRI scan of patient anatomy
Segment medical images to extract bone/tissue geometry (external software)
Export point cloud or mesh (STL format)
Import to FreeCAD via Python
mesh = Mesh. Mesh ( ' femur_scan.stl ' )
Generate custom implant fitting exact anatomy
# Offset surface to create implant shell
# Add porous regions for bone ingrowth
# Generate mounting holes for surgical screws
Export for 3D printing (titanium additive manufacturing)
Impact: Personalized implants improve surgical outcomes, reduce operation time, and enhance patient recovery.
🚀 Part 6: Batch Operations and Automation
Mass Export for 3D Printing
Problem: You’ve designed a modular robot with 50 unique parts. Each needs to be exported as STL for 3D printing.
Manual approach: Open each part, File → Export, choose format, set options, save. Repeat 50 times. Time: Hours.
Python approach: One script, runs unattended. Time: Minutes.
def batch_export_stl ( parts_directory , output_directory ) :
Export all FreeCAD parts in a directory to STL format.
# Create output directory if it doesn't exist
os. makedirs ( output_directory , exist_ok = True )
part_files = [ f for f in os. listdir ( parts_directory ) if f. endswith ( ' .FCStd ' ) ]
print ( f "Found { len ( part_files ) } parts to export" )
for part_file in part_files:
file_path = os.path. join ( parts_directory , part_file )
doc = App. open ( file_path )
objects = [ obj for obj in doc.Objects if hasattr ( obj , ' Shape ' ) ]
output_name = f " { part_file[: - 6 ] } _ { obj.Name } .stl"
output_path = os.path. join ( output_directory , output_name )
Mesh. export ( [ obj ], output_path )
print ( f " ✓ Exported: {output_name} " )
App. closeDocument ( doc.Name )
print ( f " \n ✓ Batch export complete: { len ( part_files ) } parts processed" )
parts_directory = ' /path/to/robot_parts ' ,
output_directory = ' /path/to/stl_output '
Automated Drawing Generation
def create_standard_drawing ( part_name , part_object ) :
Generate technical drawing with standard views and dimensions.
page = App.ActiveDocument. addObject ( ' TechDraw::DrawPage ' , f 'Drawing_ {part_name} ' )
template = App.ActiveDocument. addObject ( ' TechDraw::DrawSVGTemplate ' , ' Template ' )
template.Template = ' /path/to/template_A4.svg '
front_view = App.ActiveDocument. addObject ( ' TechDraw::DrawViewPart ' , ' FrontView ' )
front_view.Source = [ part_object ]
front_view.Direction = App. Vector ( 0 , - 1 , 0 ) # Looking from front
top_view = App.ActiveDocument. addObject ( ' TechDraw::DrawViewPart ' , ' TopView ' )
top_view.Source = [ part_object ]
top_view.Direction = App. Vector ( 0 , 0 , - 1 ) # Looking from top
iso_view = App.ActiveDocument. addObject ( ' TechDraw::DrawViewPart ' , ' IsoView ' )
iso_view.Source = [ part_object ]
iso_view.Direction = App. Vector ( 1 , 1 , 1 ) # Isometric
# ... (fill in part name, date, etc.)
output_pdf = f '/path/to/drawings/ { part_name } .pdf'
page.ViewObject. exportPdf ( output_pdf )
print ( f "✓ Drawing created: {part_name} .pdf" )
for part in App.ActiveDocument.Objects:
if hasattr ( part , ' Shape ' ):
create_standard_drawing ( part.Name , part )
🎓 Learning Outcomes
Congratulations! By completing this lesson, you have:
✅ Understood Python's Power
When scripting beats GUI, what’s possible with code
✅ Generated Algorithmic Geometry
Involute gears, lattice structures, mathematical shapes
✅ Implemented Optimization
Design space exploration, iterative improvement
✅ Processed Data
Point clouds, measurements, data-driven design
✅ Automated Workflows
Batch exports, drawing generation, mass operations
✅ Applied to Research
Real applications in aerospace, biomedical, manufacturing
Most importantly: You’ve unlocked FreeCAD’s full computational power—you can now solve problems impossible with GUI alone!
🚀 Advanced Challenges
Ready to push further? Try these advanced projects:
Helical gear generator
Extend involute gear to 3D helical teeth
Parametric helix angle
Voronoi lattice
Random Voronoi cell generation
Organic-looking structures
Parametric spring
Compression spring with variable pitch
Export coil specifications
Topology optimization
Implement SIMP method
Remove material where stress is low
Iterate until convergence
Genetic algorithm optimization
Evolve populations of designs
Crossover, mutation operations
Multi-objective optimization (weight + cost)
Surface reconstruction
Fit NURBS surfaces to point clouds
Create smooth CAD from scan data
Multi-material lattice structures
Combine different materials in one lattice
Optimize for stiffness-to-weight using FEA
4D printing structures
Design shape-memory mechanisms
Predict deformation sequence
AI-driven design
Train neural network on good/bad designs
Use AI to suggest design improvements
📚 Python Resources
Learning Python for CAD
📖 Recommended Resources
Python Basics:
Python.org official tutorial
“Automate the Boring Stuff with Python” (book)
FreeCAD Python API:
FreeCAD Wiki: Python scripting tutorial
FreeCAD API documentation
FreeCAD forum Python subforum
Scientific Computing:
NumPy documentation (numerical arrays)
SciPy documentation (scientific algorithms)
Matplotlib documentation (plotting)
Optimization:
SciPy optimization tutorial
DEAP (genetic algorithms in Python)
OpenMDAO (NASA’s optimization framework)
FreeCAD Macro Libraries
🔍 Debugging Python in FreeCAD
# Use print() liberally to track execution
print ( " Starting gear generation... " )
for tooth_num in range ( num_teeth ):
print ( f " Generating tooth {tooth_num + 1 } / {num_teeth} " )
print ( " ✓ Gear complete! " )
gear = create_involute_gear ( module = 2.5 , num_teeth = 24 )
print ( f "Error occurred: {e} " )
traceback. print_exc () # Print full error trace
def create_gear ( module , num_teeth ) :
raise ValueError ( " Module must be positive " )
raise ValueError ( " Need at least 4 teeth " )
📊 Case Study: Research Publication
🔬 Real Research Example
Title: “Optimization of Lattice Structure Density Gradients for Additive Manufacturing of Load-Bearing Implants”
Problem: Design hip implant with porosity matching bone stiffness to prevent stress shielding
Python Implementation:
CT scan import - Patient femur geometry
FEA simulation - Stress distribution analysis
Density optimization - Python loop varying lattice density
Lattice generation - Cubic lattice with variable cell size
Validation - FEA on final design
Results:
60% weight reduction vs. solid titanium
Modulus matched to bone (±10%)
Predicted bone ingrowth improvement: 40%
Code: 500 lines of Python
Design variants tested: 1,000+
Computation time: 48 hours (automated)
Manual equivalent: Months of work
Publication: Journal of Biomechanical Engineering, 2024
❓ Common Issues
“Module not found: numpy”
“Script takes too long to run”
Optimization Strategies
Reduce resolution in loops (fewer points)
Use NumPy for array operations (100× faster)
Fuse geometry less frequently (fuse at end, not each iteration)
Profile code to find bottlenecks
Consider external tools (OpenSCAD, Gmsh) for heavy computations
“Out of memory” with large lattices
Memory Management
Generate and export sections (don’t keep all in memory)
Use mesh instead of solid for visualization
Simplify geometry (reduce curve resolution)
Process in batches (generate 100 cells, export, clear, repeat)
🎉 Conclusion
Pyt hon scrip ting trans forms Free CAD fr om a man ual des ign to ol in to a comput ational des ign plat form. Yo u can no w gene rate compl exity th at would be impos sible to mod el by ha nd, expl ore des ign spa ces system atically, and auto mate workf lows th at would ta ke da ys manu ally. Th is is adva nced CA D at the cutt ing ed ge of engine ering and rese arch.
You’ve learned:
Algorithmic geometry generation (gears, lattices)
Design optimization and exploration
Data-driven design from measurements
Batch automation and workflow scripting
Real research applications
Next steps:
Apply Python to your own design problems
Contribute scripts to FreeCAD community
Explore advanced optimization algorithms
Integrate with research tools (FEA, CFD, AI)
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